CN104471190B - 废气涡轮增压器的叶轮 - Google Patents

废气涡轮增压器的叶轮 Download PDF

Info

Publication number
CN104471190B
CN104471190B CN201380039415.3A CN201380039415A CN104471190B CN 104471190 B CN104471190 B CN 104471190B CN 201380039415 A CN201380039415 A CN 201380039415A CN 104471190 B CN104471190 B CN 104471190B
Authority
CN
China
Prior art keywords
blade
impeller
region
thickness distribution
vane thickness
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
CN201380039415.3A
Other languages
English (en)
Chinese (zh)
Other versions
CN104471190A (zh
Inventor
M.克劳斯
T.梅伦达
B.莱迈尔
M.帕夫拉特
I.桑多尔
E.巴蒂
U.维弗
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Vitesco Technologies GmbH
Original Assignee
Continental Automotive GmbH
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Continental Automotive GmbH filed Critical Continental Automotive GmbH
Publication of CN104471190A publication Critical patent/CN104471190A/zh
Application granted granted Critical
Publication of CN104471190B publication Critical patent/CN104471190B/zh
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/14Form or construction
    • F01D5/141Shape, i.e. outer, aerodynamic form
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/14Form or construction
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D25/00Pumping installations or systems
    • F04D25/02Units comprising pumps and their driving means
    • F04D25/024Units comprising pumps and their driving means the driving means being assisted by a power recovery turbine
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/26Rotors specially for elastic fluids
    • F04D29/28Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps
    • F04D29/284Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps for compressors
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/26Rotors specially for elastic fluids
    • F04D29/28Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps
    • F04D29/30Vanes
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00Application
    • F05D2220/40Application in turbochargers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00Components
    • F05D2240/20Rotors
    • F05D2240/30Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor
    • F05D2240/301Cross-sectional characteristics
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00Geometry
    • F05D2250/70Shape
    • F05D2250/71Shape curved
    • F05D2250/711Shape curved convex
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00Geometry
    • F05D2250/70Shape
    • F05D2250/71Shape curved
    • F05D2250/712Shape curved concave

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Supercharger (AREA)
CN201380039415.3A 2012-07-24 2013-07-02 废气涡轮增压器的叶轮 Active CN104471190B (zh)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
DE102012212896.4A DE102012212896A1 (de) 2012-07-24 2012-07-24 Laufrad eines Abgasturboladers
DE102012212896.4 2012-07-24
PCT/EP2013/063958 WO2014016084A1 (de) 2012-07-24 2013-07-02 Laufrad eines abgasturboladers

Publications (2)

Publication Number Publication Date
CN104471190A CN104471190A (zh) 2015-03-25
CN104471190B true CN104471190B (zh) 2017-07-04

Family

ID=48745954

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201380039415.3A Active CN104471190B (zh) 2012-07-24 2013-07-02 废气涡轮增压器的叶轮

Country Status (7)

Country Link
US (1) US10253633B2 (enrdf_load_html_response)
EP (1) EP2877701B1 (enrdf_load_html_response)
CN (1) CN104471190B (enrdf_load_html_response)
BR (1) BR112015001398B8 (enrdf_load_html_response)
DE (1) DE102012212896A1 (enrdf_load_html_response)
IN (1) IN2014DN10346A (enrdf_load_html_response)
WO (1) WO2014016084A1 (enrdf_load_html_response)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11421702B2 (en) 2019-08-21 2022-08-23 Pratt & Whitney Canada Corp. Impeller with chordwise vane thickness variation

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2960462B1 (en) * 2013-02-21 2019-01-09 Mitsubishi Heavy Industries, Ltd. Turbine wheel for a radial turbine
JP5705945B1 (ja) * 2013-10-28 2015-04-22 ミネベア株式会社 遠心式ファン
DE102014004745A1 (de) * 2014-04-01 2015-10-01 Daimler Ag Turbinenrad für eine Turbine, insbesondere eines Abgasturboladers
JP6372207B2 (ja) * 2014-07-08 2018-08-15 株式会社豊田中央研究所 コンプレッサに用いるインペラおよびターボチャージャ
JP2016084751A (ja) * 2014-10-27 2016-05-19 三菱重工業株式会社 インペラ、遠心式流体機械、及び流体装置
US9845684B2 (en) * 2014-11-25 2017-12-19 Pratt & Whitney Canada Corp. Airfoil with stepped spanwise thickness distribution
JP6210459B2 (ja) * 2014-11-25 2017-10-11 三菱重工業株式会社 インペラ、及び回転機械
US20160245297A1 (en) * 2015-02-23 2016-08-25 Howden Roots Llc Impeller comprising variably-dimensioned fillet to secure blades and compressor comprised thereof
DE102015205998A1 (de) * 2015-04-02 2016-10-06 Ford Global Technologies, Llc Aufgeladene Brennkraftmaschine mit zweiflutiger Turbine und gruppierten Zylindern
JP2017193982A (ja) * 2016-04-19 2017-10-26 本田技研工業株式会社 コンプレッサ
US11346226B2 (en) * 2016-12-23 2022-05-31 Borgwarner Inc. Turbocharger and turbine wheel
CN107869359A (zh) * 2017-12-01 2018-04-03 无锡宇能选煤机械厂 流线型厚叶片涡轮增压器转子轴
CN111699323B (zh) * 2018-06-11 2021-12-21 三菱重工发动机和增压器株式会社 旋转叶片以及具备该旋转叶片的离心压缩机
US10465522B1 (en) * 2018-10-23 2019-11-05 Borgwarner Inc. Method of reducing turbine wheel high cycle fatigue in sector-divided dual volute turbochargers
US11125154B2 (en) * 2019-10-25 2021-09-21 Pratt & Whitney Canada Corp. Centrifugal impeller for gas turbine engine
JP7409246B2 (ja) * 2020-07-14 2024-01-09 株式会社デンソー ターボファン
JP7749974B2 (ja) * 2021-08-12 2025-10-07 株式会社Ihi インペラ、および、遠心圧縮機

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2469458A (en) * 1945-09-24 1949-05-10 United Aircraft Corp Blade form for supercharger impellers
GB941344A (en) * 1961-11-06 1963-11-13 Rudolph Birmann Improvements in or relating to a centripetal turbine
GB1053509A (enrdf_load_html_response) * 1963-10-25
NO146029C (no) * 1976-08-11 1982-07-14 Kongsberg Vapenfab As Impellerelement i et radialgassturbinhjul
US4587700A (en) * 1984-06-08 1986-05-13 The Garrett Corporation Method for manufacturing a dual alloy cooled turbine wheel
US5408747A (en) * 1994-04-14 1995-04-25 United Technologies Corporation Compact radial-inflow turbines
DE19612396C2 (de) * 1996-03-28 1998-02-05 Univ Dresden Tech Schaufelblatt mit unterschiedlich ausgebildeten Profilquerschnitten
SE525219C2 (sv) 2003-05-15 2004-12-28 Volvo Lastvagnar Ab Turboladdarsystem för en förbränningsmotor där båda kompressorstegen är av radialtyp med kompressorhjul försedda med bakåtsvepta blad
CN100406746C (zh) 2004-03-23 2008-07-30 三菱重工业株式会社 离心压缩机及叶轮的制造方法
JP4545009B2 (ja) * 2004-03-23 2010-09-15 三菱重工業株式会社 遠心圧縮機
WO2009065030A2 (en) * 2007-11-16 2009-05-22 Borgwarner Inc. Low blade frequency titanium compressor wheel
US20110020152A1 (en) 2008-04-08 2011-01-27 Volvo Lastvagnar Ab Compressor
DE102008059874A1 (de) 2008-12-01 2010-06-02 Continental Automotive Gmbh Geometrische Gestaltung der Laufradschaufeln eines Turboladers
US8172511B2 (en) * 2009-05-04 2012-05-08 Hamilton Sunstrand Corporation Radial compressor with blades decoupled and tuned at anti-nodes

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11421702B2 (en) 2019-08-21 2022-08-23 Pratt & Whitney Canada Corp. Impeller with chordwise vane thickness variation

Also Published As

Publication number Publication date
BR112015001398B8 (pt) 2023-04-18
CN104471190A (zh) 2015-03-25
DE102012212896A1 (de) 2014-02-20
BR112015001398B1 (pt) 2021-09-28
WO2014016084A1 (de) 2014-01-30
US10253633B2 (en) 2019-04-09
EP2877701A1 (de) 2015-06-03
US20150204195A1 (en) 2015-07-23
EP2877701B1 (de) 2017-05-10
IN2014DN10346A (enrdf_load_html_response) 2015-08-07
BR112015001398A2 (pt) 2017-07-04

Similar Documents

Publication Publication Date Title
CN104471190B (zh) 废气涡轮增压器的叶轮
US7255530B2 (en) Vane and throat shaping
CN102296995B (zh) 用于向涡轮引导废气的叶片
JP4881390B2 (ja) ターボチャージャ
JP4923073B2 (ja) 遷音速翼
US9951793B2 (en) Ported shroud geometry to reduce blade-pass noise
JP5300874B2 (ja) 非軸対称プラットフォームならびに外輪上の陥没および突起を備えるブレード
JP5629177B2 (ja) タービン翼形部
US9188017B2 (en) Airfoil assembly with paired endwall contouring
US9004865B2 (en) Blade with non-axisymmetric platform
JP2015183691A (ja) ガスタービンブレード
JP6110942B2 (ja) 流体機械の羽根車
EP1270872A1 (en) Gas turbine engine
JP6710271B2 (ja) 回転機械翼
JP7104379B2 (ja) 軸流型のファン、圧縮機及びタービンの翼の設計方法、並びに、当該設計により得られる翼
CN105814279A (zh) 废气涡轮增压器
US9869184B2 (en) Gas turbine blade
WO2014203372A1 (ja) 半径流入式軸流タービン及びターボチャージャ
CN108952820B (zh) 具有降低的惯量的涡轮机叶轮
JP5351637B2 (ja) 翼体および回転機械
JP2021139316A (ja) ターボ機械の羽根の設計方法
CN106460646A (zh) 涡轮外壳、涡轮、用于铸造涡轮外壳的型芯、以及涡轮外壳的制造方法
US20180142557A1 (en) Turbocharger impeller blade stiffeners and manufacturing method
CN104747240A (zh) 小型涡轮增压器的转子系统
RU2632350C2 (ru) Выпрямитель газотурбинного двигателя с лопатками улучшенного профиля

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant
TR01 Transfer of patent right
TR01 Transfer of patent right

Effective date of registration: 20230428

Address after: Regensburg, Germany

Patentee after: WeiPai Technology Co.,Ltd.

Address before: Hannover

Patentee before: CONTINENTAL AUTOMOTIVE GmbH